All-crack remanufacturability evaluation for blade with surface crack
Remanufacturing repair has been applied as a promising technology to extend the fatigue life of damaged components. For the compressor blade with shallow surface crack, crack can be directly repaired by crack arrest and healing technology. However, for the blade with macrosurface crack, a surface no...
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| Veröffentlicht in: | Journal of the Brazilian Society of Mechanical Sciences and Engineering 2021-09, Vol.43 (9), Article 434 |
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| container_title | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
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| creator | Ding, Mingchao Zhang, Yuanliang |
| description | Remanufacturing repair has been applied as a promising technology to extend the fatigue life of damaged components. For the compressor blade with shallow surface crack, crack can be directly repaired by crack arrest and healing technology. However, for the blade with macrosurface crack, a surface notch will be generated by crack grinding process and then repaired by laser cladding technology. Therefore, there are essential differences in the remanufacturability evaluation methods for blade with shallow cracks or macrocracks. In this study, the remanufacturability evaluation methods that can be suitable for the blade with any depth surface crack are studied. Firstly, remanufacturability evaluation for shallow crack is introduced based on fracture mechanics. Secondly, remanufacturability evaluation based on surface notch is established for the blade with macrocrack. It consists of preliminary remanufacturability evaluation, remanufacturability evaluation based on residual fatigue life and remanufacturability evaluation based on fatigue damage. Finally, combined with the remanufacturability evaluation for shallow crack and macrocrack, all-crack remanufacturability evaluation is proposed that suitable for the blade with any depth surface cracks. With the assistance of all-crack remanufacturability evaluation, the potential fatigue performance of cracked blades can be reused furthest and reduce the waste of resources as much as possible. |
| doi_str_mv | 10.1007/s40430-021-03149-4 |
| format | Article |
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For the compressor blade with shallow surface crack, crack can be directly repaired by crack arrest and healing technology. However, for the blade with macrosurface crack, a surface notch will be generated by crack grinding process and then repaired by laser cladding technology. Therefore, there are essential differences in the remanufacturability evaluation methods for blade with shallow cracks or macrocracks. In this study, the remanufacturability evaluation methods that can be suitable for the blade with any depth surface crack are studied. Firstly, remanufacturability evaluation for shallow crack is introduced based on fracture mechanics. Secondly, remanufacturability evaluation based on surface notch is established for the blade with macrocrack. It consists of preliminary remanufacturability evaluation, remanufacturability evaluation based on residual fatigue life and remanufacturability evaluation based on fatigue damage. Finally, combined with the remanufacturability evaluation for shallow crack and macrocrack, all-crack remanufacturability evaluation is proposed that suitable for the blade with any depth surface cracks. With the assistance of all-crack remanufacturability evaluation, the potential fatigue performance of cracked blades can be reused furthest and reduce the waste of resources as much as possible.</description><identifier>ISSN: 1678-5878</identifier><identifier>EISSN: 1806-3691</identifier><identifier>DOI: 10.1007/s40430-021-03149-4</identifier><language>eng</language><publisher>Berlin/Heidelberg: Springer Berlin Heidelberg</publisher><subject>Compressor blades ; Crack arrest ; Crack propagation ; Damage ; Engineering ; Fatigue cracks ; Fatigue failure ; Fatigue life ; Fracture mechanics ; Laser beam cladding ; Mechanical Engineering ; Remanufacturing ; Surface cracks ; Technical Paper</subject><ispartof>Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2021-09, Vol.43 (9), Article 434</ispartof><rights>The Brazilian Society of Mechanical Sciences and Engineering 2021</rights><rights>The Brazilian Society of Mechanical Sciences and Engineering 2021.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-d1b0396549f327601f960ef8dd7f273ae518ee31f3fb34c28da9a4568515c8dd3</citedby><cites>FETCH-LOGICAL-c319t-d1b0396549f327601f960ef8dd7f273ae518ee31f3fb34c28da9a4568515c8dd3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s40430-021-03149-4$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s40430-021-03149-4$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Ding, Mingchao</creatorcontrib><creatorcontrib>Zhang, Yuanliang</creatorcontrib><title>All-crack remanufacturability evaluation for blade with surface crack</title><title>Journal of the Brazilian Society of Mechanical Sciences and Engineering</title><addtitle>J Braz. Soc. Mech. Sci. Eng</addtitle><description>Remanufacturing repair has been applied as a promising technology to extend the fatigue life of damaged components. For the compressor blade with shallow surface crack, crack can be directly repaired by crack arrest and healing technology. However, for the blade with macrosurface crack, a surface notch will be generated by crack grinding process and then repaired by laser cladding technology. Therefore, there are essential differences in the remanufacturability evaluation methods for blade with shallow cracks or macrocracks. In this study, the remanufacturability evaluation methods that can be suitable for the blade with any depth surface crack are studied. Firstly, remanufacturability evaluation for shallow crack is introduced based on fracture mechanics. Secondly, remanufacturability evaluation based on surface notch is established for the blade with macrocrack. It consists of preliminary remanufacturability evaluation, remanufacturability evaluation based on residual fatigue life and remanufacturability evaluation based on fatigue damage. Finally, combined with the remanufacturability evaluation for shallow crack and macrocrack, all-crack remanufacturability evaluation is proposed that suitable for the blade with any depth surface cracks. With the assistance of all-crack remanufacturability evaluation, the potential fatigue performance of cracked blades can be reused furthest and reduce the waste of resources as much as possible.</description><subject>Compressor blades</subject><subject>Crack arrest</subject><subject>Crack propagation</subject><subject>Damage</subject><subject>Engineering</subject><subject>Fatigue cracks</subject><subject>Fatigue failure</subject><subject>Fatigue life</subject><subject>Fracture mechanics</subject><subject>Laser beam cladding</subject><subject>Mechanical Engineering</subject><subject>Remanufacturing</subject><subject>Surface cracks</subject><subject>Technical Paper</subject><issn>1678-5878</issn><issn>1806-3691</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kD1PwzAQhi0EEqXwB5giMRvu4o84Y1UVilSJBWbLcWxISZNiJ6D-e0yDxMZ0NzzPe7qXkGuEWwQo7iIHzoBCjhQY8pLyEzJDBZIyWeJp2mWhqFCFOicXMW4BWC6kmJHVom2pDca-Z8HtTDd6Y4cxmKppm-GQuU_TjmZo-i7zfciq1tQu-2qGtyyOIaEuO7qX5MybNrqr3zknL_er5-Wabp4eHpeLDbUMy4HWWAErpeClZ3khAX0pwXlV14XPC2acQOUcQ898xbjNVW1Kw4VUAoVNFJuTmyl3H_qP0cVBb_sxdOmkTu9wFKAAE5VPlA19jMF5vQ_NzoSDRtA_dempLp3q0se6NE8Sm6SY4O7Vhb_of6xvo49s-w</recordid><startdate>20210901</startdate><enddate>20210901</enddate><creator>Ding, Mingchao</creator><creator>Zhang, Yuanliang</creator><general>Springer Berlin Heidelberg</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20210901</creationdate><title>All-crack remanufacturability evaluation for blade with surface crack</title><author>Ding, Mingchao ; Zhang, Yuanliang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-d1b0396549f327601f960ef8dd7f273ae518ee31f3fb34c28da9a4568515c8dd3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Compressor blades</topic><topic>Crack arrest</topic><topic>Crack propagation</topic><topic>Damage</topic><topic>Engineering</topic><topic>Fatigue cracks</topic><topic>Fatigue failure</topic><topic>Fatigue life</topic><topic>Fracture mechanics</topic><topic>Laser beam cladding</topic><topic>Mechanical Engineering</topic><topic>Remanufacturing</topic><topic>Surface cracks</topic><topic>Technical Paper</topic><toplevel>online_resources</toplevel><creatorcontrib>Ding, Mingchao</creatorcontrib><creatorcontrib>Zhang, Yuanliang</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ding, Mingchao</au><au>Zhang, Yuanliang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>All-crack remanufacturability evaluation for blade with surface crack</atitle><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle><stitle>J Braz. Soc. Mech. Sci. Eng</stitle><date>2021-09-01</date><risdate>2021</risdate><volume>43</volume><issue>9</issue><artnum>434</artnum><issn>1678-5878</issn><eissn>1806-3691</eissn><abstract>Remanufacturing repair has been applied as a promising technology to extend the fatigue life of damaged components. For the compressor blade with shallow surface crack, crack can be directly repaired by crack arrest and healing technology. However, for the blade with macrosurface crack, a surface notch will be generated by crack grinding process and then repaired by laser cladding technology. Therefore, there are essential differences in the remanufacturability evaluation methods for blade with shallow cracks or macrocracks. In this study, the remanufacturability evaluation methods that can be suitable for the blade with any depth surface crack are studied. Firstly, remanufacturability evaluation for shallow crack is introduced based on fracture mechanics. Secondly, remanufacturability evaluation based on surface notch is established for the blade with macrocrack. It consists of preliminary remanufacturability evaluation, remanufacturability evaluation based on residual fatigue life and remanufacturability evaluation based on fatigue damage. Finally, combined with the remanufacturability evaluation for shallow crack and macrocrack, all-crack remanufacturability evaluation is proposed that suitable for the blade with any depth surface cracks. With the assistance of all-crack remanufacturability evaluation, the potential fatigue performance of cracked blades can be reused furthest and reduce the waste of resources as much as possible.</abstract><cop>Berlin/Heidelberg</cop><pub>Springer Berlin Heidelberg</pub><doi>10.1007/s40430-021-03149-4</doi></addata></record> |
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| language | eng |
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| source | Springer Nature - Complete Springer Journals |
| subjects | Compressor blades Crack arrest Crack propagation Damage Engineering Fatigue cracks Fatigue failure Fatigue life Fracture mechanics Laser beam cladding Mechanical Engineering Remanufacturing Surface cracks Technical Paper |
| title | All-crack remanufacturability evaluation for blade with surface crack |
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